CN206095799U - Can realize that each is to testing system who draws - Google Patents
Can realize that each is to testing system who draws Download PDFInfo
- Publication number
- CN206095799U CN206095799U CN201621137867.2U CN201621137867U CN206095799U CN 206095799 U CN206095799 U CN 206095799U CN 201621137867 U CN201621137867 U CN 201621137867U CN 206095799 U CN206095799 U CN 206095799U
- Authority
- CN
- China
- Prior art keywords
- sample box
- cylinder
- pilot system
- revolution driving
- testing system
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Landscapes
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
Abstract
The utility model belongs to the technical field of the synthetic material mechanical properties test, particularly, involve a can realize that each is to testing system who draws. This testing system includes test bench, automatically controlled cabinet, touch -sensitive screen, servo motor, electronic jar, draw press sensor, cylinder, cylinder loading board, slewing bearing, sample box loading board, go up sample box, sample box, step motor, swing drives, synchronal rotary device, anchor clamps, geogrid, servo motor 0 down. Compared with the prior art, the can realize that each is to testing system who draws problem of effectively having avoided existing testing system test value and geosynthetic material actual stress characteristic seriously not to be inconsistent, solved the potential safety hazard that exists among the geosynthetic material engineering application.
Description
Technical field
This utility model belongs to synthetic material mechanics performance testing technology field, it particularly relates to arrive one kind can realize
Each pilot system to drawing.
Background technology
Modern reinforced soil technical is that French engineer HemiVidal was proposed first in 1966, and in 80 years 20th century
In generation, just introduces China, is widely applied in water conservancy, railway, highway, harbour and architectural engineering, solves many buildings
Technical barrier in engineering, obtains good Social and economic benef@, thus the technology is flourished.
In recent decades, different types of muscle material (from high molecular polymer of the metal of low ductility to high ductility) is used for
In earth structure, and high molecular polymer muscle material applies then wider in Reinforced Material with Clay Engineering.It is generally believed that less to rigidity
With direct shear friction test, geosynthetics, determines that its intensive parameter relatively meets reality;The material larger to rigidity, then using drawing
Pull out test preferably.American scholar McGown is proposed, for various earth structures, play reinforced action is all geotechnological synthesis
The resistance to plucking resistance of material, he determines boundary strength with pull-out test at opinion, while obtaining the stress-strain for being embedded in muscle material in soil
Relation.French Schdsser thinks that the advantage of pull-out test is that test result can reflect that the soil body cuts swollen and densification state automatically,
And preferably simulate working condition of the muscle material in soil.Field actual measurement results are it was demonstrated that pull-out test can simulate reinforced earth knot really
Reinforcement behavior in structure, provides a kind of reliable method to obtain suitable design parameter, and GSZ is considered as resistance
Only drawing destroys one of most effective muscle material.
The factor of pull-out test result is affected to have a lot, be to be produced by pilot system below at 2 points:One is geotechnological synthesis
Rubbing action between material and box (case) wall, it increases applied pulling capacity, virtually enhances geosynthetics
Drawing characteristic;Two is drawing speed, the unstable estimation that will also result in geosynthetics drawing characteristic of drawing speed
Deviation.The purpose of test is the interface mechanical characteristic between studying geosynthetics and banketing, it is necessary in accurate recording test
The horizontal displacement of the normal pressure, pulling capacity and the geosynthetics that are applied.Therefore, the precision of pilot system is most important.
Simultaneously, it is also desirable to consider geosynthetics and receive the performance under different directions load whether different, should during design
Take the minima in all directions.
In sum, the geosynthetics that obtains of test and the interface mechanical characteristic between banketing often are better than engineering
There is larger hidden danger, seriously threaten engineering in geosynthetics and the interface mechanical characteristic for banketing in practice, its security performance
Quality and people life property safety.
Utility model content
To solve above-mentioned technical problem, this utility model is there is provided a kind of test data is accurate, process control is good, operation
Easy can realize each pilot system to drawing.
It is described in the utility model it is a kind of can realize each pilot system to drawing, the pilot system include testing stand 1,
Electrical control cubicles 2, touch screen 3, servomotor 4, electric cylinder 5, tension-compression sensor 6, cylinder 7, cylinder loading plate 8, pivoting support 9, examination
Sample box loading plate 10, upper sample box 11, lower sample box 12, motor 13, revolution driving 14, synchronous rotating device 15, fixture
16th, GSZ 17 and piston rod 18;The electrical control cubicles 2 and electric cylinder 5 are arranged on 1 side of testing stand, and left and right is arranged;It is described
Electrical control cubicles 2 are furnished with touch screen 3;The electric cylinder 5 is driven using servomotor 4, and is connected with 6 one end of tension-compression sensor, the drawing
6 other end of pressure sensor is connected with fixture 16;Revolution driving 14 is provided with 1 opposite side of the testing stand, with lower sample box 12
It is coaxial fixed;Upper sample box 11 and pivoting support 9 are coaxial fixed, through being placed on sample box loading plate 10;Upper sample box 11
It is fixedly connected by synchronous rotating device 15 with lower sample box 12, drives revolution driving 14 to rotate by motor 13, and then
Sample box 11 is made with lower 12 synchronous rotary of sample box;The cylinder 7 is fixed on cylinder loading plate 8, and with upper sample box 11,
Lower sample box 12, revolution driving 14 are concentric;The piston rod 18 is connected to 7 lower end of cylinder;GSZ 17 is placed in lower sample box
12 upper surface;The electrical control cubicles 1 are connected with servomotor 4 and cylinder 6 respectively.
It is described in the utility model it is a kind of can realize each pilot system to drawing, the servomotor 4 drives electric cylinder
5, it is connected with fixture 16 by tension-compression sensor 6, there is provided horizontal pulling capacity and horizontal displacement, velocity accuracy 0.1mm/min;Utilize
PLC reads motor encoder umber of pulse, calculates displacement, displacement accuracy 0.01mm in real time.
It is described in the utility model a kind of to realize each pilot system to drawing, the upper sample box 11 and lower sample box
12 is hollow cylinder, and consistent size, and internal diameter is more than or equal to 200mm, highly more than or equal to 50mm.
It is described in the utility model it is a kind of can realize each pilot system to drawing, the upper sample box 11 is adjusted by installing
Gap of the whole pad adjustment with lower sample box 12 in vertical direction.
It is described in the utility model it is a kind of can realize each pilot system to drawing, the revolution driving 14 is using stepping electricity
Machine 13 drives rotation, and the anglec of rotation is 0-360 °.
In this utility model, servomotor drives electric cylinder to provide pulling capacity and horizontal displacement, speed displacement high precision,
Range of accommodation is wide, has been improved the accuracy of test data;Meanwhile, drive revolution driving to rotate by motor, and upper,
Lower sample box is fixed by synchronous rotating device, is made upper and lower sample box synchronous rotary, is realized 0-360 ° of drawing;Using regulation
Pad adjusts the gap of upper and lower sample box, eliminates impact of the sample box surface with the frictional force of GSZ to result of the test;
Normal stress is provided by cylinder, pressure value can be read at any time by pressure gauge, and concentric with upper and lower sample box normal direction, made
Soil sample is more uniformly stressed, and during calculating, theoretical value can more reflect real working condition closer to actual value.
Compared with prior art, it is described in the utility model can realize it is each effectively prevent to the pilot system of drawing it is existing
Pilot system test value and the problem of geosynthetics actual loading characteristic grave fault, solve geosynthetics engineering
The potential safety hazard using present in.
Description of the drawings
Fig. 1:The plane structure chart of pilot system described in the utility model;Fig. 2:Draw power is dialled with drawing group displacement changing curve;
1- testing stands;2- electrical control cubicles;3- touch screens;4- servomotors;5- electric cylinders;6- tension-compression sensors;7- cylinders;8- cylinders are carried
Plate;9- pivoting supports;10- sample box loading plates;The upper sample boxs of 11-;Sample box under 12-;13- motors;14- revolutions are driven
It is dynamic;15- synchronous rotating devices;16- fixtures;17- GSZs;18- cylinder pistons.
Specific embodiment
Can realize each doing into one to the pilot system of drawing to described in the utility model with reference to specific embodiment
Step explanation, but protection domain of the present utility model is not limited to this.
Embodiment 1
It is a kind of to realize each pilot system to drawing, including testing stand 1, electrical control cubicles 2, touch screen 3, servomotor 4, electricity
Dynamic cylinder 5, tension-compression sensor 6, cylinder 7, cylinder loading plate 8, pivoting support 9, sample box loading plate 10, upper sample box 11, lower examination
Sample box 12, motor 13, revolution driving 14, synchronous rotating device 15, fixture 16, GSZ 17 and piston rod 18;It is described
Electrical control cubicles 2 and electric cylinder 5 are arranged on 1 side of testing stand, and left and right is arranged;Electrical control cubicles 2 are furnished with touch screen 3;Electric cylinder 5 is adopted and is watched
Take motor 4 to drive, and be connected with 6 one end of tension-compression sensor, 6 other end of tension-compression sensor is connected with fixture 16;The test
Revolution driving 14 is provided with 1 opposite side of platform, it is coaxial with lower sample box 12 fixed;Upper sample box 11 is coaxial with pivoting support 9 solid
It is fixed, through being placed on sample box loading plate 10;Upper sample box 11 is fixed by synchronous rotating device 15 with lower sample box 12 and is connected
Connect, drive revolution driving 14 to rotate by motor 13, and then sample box 11 is made with lower 12 synchronous rotary of sample box;It is described
Cylinder 7 is fixed on cylinder loading plate 8, and concentric with upper sample box 11, lower sample box 12, revolution driving 14;Piston rod 18 connects
It is connected on 7 lower end of cylinder;GSZ 17 is placed in the upper surface of lower sample box 12;The electrical control cubicles 1 respectively with servomotor 4 and
Cylinder 6 is connected.
The servomotor 4 drive electric cylinder 5, be connected with fixture 16 by tension-compression sensor 6, there is provided horizontal pulling capacity and
Horizontal displacement, velocity accuracy 0.1mm/min;Motor encoder umber of pulse is read using PLC, displacement, displacement accuracy is calculated in real time
0.01mm.The upper sample box 11 and lower sample box 12 are hollow cylinder, and consistent size, and internal diameter is more than or equal to 200mm, high
Degree is more than or equal to 50mm.The upper sample box 11 by mounting and adjusting pad adjust and lower sample box 12 in vertical direction between
Gap.The revolution driving 14 drives rotation using motor 13, and the anglec of rotation is 0-360 °.
It is controlled from Omron CP1H-Y series of PLC in electrical control cubicles, is furnished with NB array of touch screens, and has respectively some
Display lamp and button;Electric cylinder is using thatch DMC75-0560-1500-020-31 advanced in years;Servo motor model number is peace river SGMJV-
02A3A61;Tension-compression sensor is serial using high spirit CFBLS-1;CS1B200-250 of the cylinder using SMC;Revolution driving adopts ten thousand
Up to SE12-78-H-25R, pivoting support adopts Wanda 010.12.280F;Motor reaches 86BYG350-114 using letter is precious.Gas
Cylinder loading plate adopts steel plate with sample box loading plate, and size is 700 × 500 × 14mm;Upper sample box is cylinder with lower sample box
Shape, internal diameter 200mm, thickness 5mm;Fixture is Wedge gripping;GSZ is circle, its diameter 220mm.
The implementation that each pilot system to drawing can be realized described in the utility model, the implementation concrete steps
For:
A) by GSZ 17, circular in cross-section is cut, diameter is bigger than upper sample box 11,12 internal diameter of lower sample box
20mm;
B) 12 filling test soil sample of sample box be compacted downwards, compactness regarding actual condition depending on, compacting get well after by its
It is fixed in revolution driving 14;Upper sample box 11 is passed through into sample box loading plate 8 and is connected with pivoting support 9, according to soil
The thickness addition adjust pad of work grid 17, makes the gap between sample box 11 and lower sample box 12 be slightly larger than GSZ 17
Thickness;
C) GSZ 17 is placed on the upper surface of lower sample box 12, it is ensured that GSZ 17 full of upper sample box 11 with
The coincidence section of lower sample box 12;
Electric cylinder 5 is stretched out by D) operation touch-screen 3, control servomotor 4, reaches on-test specified location, by folder
GSZ 17 is fixedly clamped by tool 16;
E) operation touch-screen 3, adjust 7 pressure of cylinder, and by piston rod (18), sample box (11) applies normal stress, gas upwards
Pressure degree of regulation is 0.1kPa, and in 2.5 hours, air pressure is dropped by less than 0.5%, and regulation air pressure is 300kPa;
F) operation touch-screen 3, set horizontal displacement-pattern as 1mm/min;
G test) is proceeded by, by the rotating speed of PLC Real-time Collections servomotor 4, and is remembered according to encoder count feedback
Record real-time displacement.Touch screen shows in real time and records normal stress and horizontal pulling capacity, and sample frequency is 1Hz, until geotechnological lattice
Grid 17 be completely pulled out of or terminate when breaking test;
H) by 7 pressure release of cylinder, lower upper sample box 11 is removed, checks whether GSZ 17 is damaged;Weak damage, then need
Change GSZ 17 and re-start step A to G;If not being damaged, GSZ 17 is put back to before pull-out test
Initial position;
I) upper sample box 11 is reinstalled, by fixture 16 unclamp and operation touch-screen 3 to be retreated to electric cylinder 5 former
Point, control motor 13 make revolution driving rotate specified angle;
J) control electric cylinder 5 and come back to test origin, then the GSZ 17 of specified angle will be had turned to fixture 16
Retighten, re-start step D to G.Pull-out test has been carried out to GSZ 17 by different directions thus.
Fig. 2 is the GSZ for obtaining at the conditions of the experiments described above drawing displacement and pulling capacity under 0 ° with 45° angle degree
Change curve.It can be seen that GSZ is inconsistent with the draft in 45 ° of directions at 0 °, i.e., mechanical property is not
Equally.As can be seen that the anisotropy of geosynthetics ought not considered, engineering is carried out according to geosynthetics nominal performance
During design, requirement may be unsatisfactory for and be unsatisfactory for engineering actual demand, seriously threaten construction quality and people life property safety.
In sum, this utility model has taken into full account the anisotropy of GSZ performance, more accurate can must assess geotechnological synthesis
The performance of material, solves potential safety hazard present in engineer applied.
Claims (5)
1. it is a kind of to realize each pilot system to drawing, it is characterised in that the pilot system includes testing stand (1), automatically controlled
Cabinet (2), touch screen (3), servomotor (4), electric cylinder (5), tension-compression sensor (6), cylinder (7), cylinder loading plate (8), return
Turn supporting (9), sample box loading plate (10), upper sample box (11), lower sample box (12), motor (13), revolution driving
(14), synchronous rotating device (15), fixture (16), GSZ (17) and piston rod (18);Electrical control cubicles (2) and electronic
Cylinder (5) is arranged on testing stand (1) side, and left and right is arranged;Electrical control cubicles (2) are furnished with touch screen (3);Electric cylinder (5) is using servo electricity
Machine (4) drives, and is connected with tension-compression sensor (6) one end, and the tension-compression sensor (6) other end is connected with fixture (16);It is described
Revolution driving (14) is provided with testing stand (1) opposite side, it is coaxial with lower sample box (12) fixed;Upper sample box (11) and revolution
Supporting (9) is coaxially fixed, through being placed on sample box loading plate (10);Upper sample box (11) is with lower sample box (12) by same
Step slewing equipment (15) is fixedly connected, and drives revolution driving (14) rotation by motor (13), and then makes sample box
(11) with lower sample box (12) synchronous rotary;The cylinder (7) is fixed on cylinder loading plate (8), and with upper sample box (11),
Lower sample box (12), revolution driving (14) are with one heart;Piston rod (18) is connected to cylinder (7) lower end;GSZ (17) is placed in down
The upper surface of sample box (12);The electrical control cubicles (1) are connected with servomotor (4) and cylinder (6) respectively.
2. it is according to claim 1 to realize each pilot system to drawing, it is characterised in that the servomotor (4)
Electric cylinder (5) is driven, is connected with fixture (16) by tension-compression sensor (6), there is provided horizontal pulling capacity and horizontal displacement, speed essence
Degree 0.1mm/min;Motor encoder umber of pulse is read using PLC, displacement, displacement accuracy 0.01mm is calculated in real time.
3. it is according to claim 1 to realize each pilot system to drawing, it is characterised in that the upper sample box (11)
It is hollow cylinder with lower sample box (12), and consistent size, internal diameter is more than or equal to 200mm, highly more than or equal to 50mm.
4. it is according to claim 1 to realize each pilot system to drawing, it is characterised in that the upper sample box (11)
Gap with lower sample box (12) in vertical direction is adjusted by mounting and adjusting pad.
5. it is according to claim 1 to realize each pilot system to drawing, it is characterised in that the revolution driving (14)
Driven using motor (13) and rotated, the anglec of rotation is 0-360 °.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201621137867.2U CN206095799U (en) | 2016-10-19 | 2016-10-19 | Can realize that each is to testing system who draws |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201621137867.2U CN206095799U (en) | 2016-10-19 | 2016-10-19 | Can realize that each is to testing system who draws |
Publications (1)
Publication Number | Publication Date |
---|---|
CN206095799U true CN206095799U (en) | 2017-04-12 |
Family
ID=59975753
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201621137867.2U Expired - Fee Related CN206095799U (en) | 2016-10-19 | 2016-10-19 | Can realize that each is to testing system who draws |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN206095799U (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106289987A (en) * | 2016-10-19 | 2017-01-04 | 山西省交通科学研究院 | A kind of can realize each pilot system to drawing and implementation thereof |
CN107144466A (en) * | 2017-05-23 | 2017-09-08 | 山东大学 | Determine the device and method of earth working material nonlinear mechanics character in pull-out test |
CN112362213A (en) * | 2020-12-07 | 2021-02-12 | 东莞华贝电子科技有限公司 | Magnet drawing force testing device |
-
2016
- 2016-10-19 CN CN201621137867.2U patent/CN206095799U/en not_active Expired - Fee Related
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106289987A (en) * | 2016-10-19 | 2017-01-04 | 山西省交通科学研究院 | A kind of can realize each pilot system to drawing and implementation thereof |
CN107144466A (en) * | 2017-05-23 | 2017-09-08 | 山东大学 | Determine the device and method of earth working material nonlinear mechanics character in pull-out test |
CN107144466B (en) * | 2017-05-23 | 2019-12-20 | 山东大学 | Device and method for determining nonlinear mechanical behavior of geotechnical material in drawing test |
CN112362213A (en) * | 2020-12-07 | 2021-02-12 | 东莞华贝电子科技有限公司 | Magnet drawing force testing device |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP2833119B1 (en) | Dynamics performance testing system | |
CN206095799U (en) | Can realize that each is to testing system who draws | |
CN108613885B (en) | Indoor test method for simulating pile side post grouting | |
CN201145658Y (en) | Portable on site and indoor dual-purpose direct shear test instrument | |
CN106289987A (en) | A kind of can realize each pilot system to drawing and implementation thereof | |
CN201795963U (en) | System for testing fracture of concrete | |
CN105319130B (en) | A kind of jointed rock mass pressure of testing cuts the test method of performance | |
WO2019223017A1 (en) | Large-size multifunctional interface power shear tester and test method | |
CN105223080B (en) | Evaluation method for jointed rock performance and bolting and grouting effects under compression-shear condition | |
CN203066126U (en) | Test device for simulating vertical tension-compression load effect on pile foundations | |
CN104344789A (en) | System and method for monitoring member deflection in bearing capacity test | |
CN114324010B (en) | Rock mass structural plane multidirectional dynamic shear mechanics testing system based on vibration table principle | |
CN104374650A (en) | Testing device and method for testing static force shear property between tubular pile and grouting soil body | |
CN111456117A (en) | Pile forming loading model test device and method for stiff composite pile | |
CN109883822B (en) | Horizontal static load test device and method for CT scanning | |
CN110646343B (en) | Confining pressure adjustable anchor rod test piece uplift resistance test device and method | |
CN108343099B (en) | Device and method for testing horizontal bearing capacity of pile under dynamic wave pressure | |
CN104132802A (en) | Vertical large-stroke loading device and test method for centrifugation model test | |
CN209690049U (en) | A kind of horizontal dead load test device for CT scan | |
CN209211512U (en) | A kind of vertical hammering load pile foundation model test apparatus of calcareous sand | |
KR100397072B1 (en) | Large Cyclic Triaxial Testing Apparatus | |
CN206627381U (en) | It is a kind of to be used for soil and the visualization laminar shear box of structure interface shearing test | |
CN113982048B (en) | Pile unit multidirectional coupling loading test device | |
CN215296993U (en) | Multi-connected rock-soil in-situ shear testing device for full-stress path tracking | |
CN204461981U (en) | A kind of pile tube Vertical Static Loading Test visual Simulation device |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170412 Termination date: 20181019 |
|
CF01 | Termination of patent right due to non-payment of annual fee |